高可压缩横向射流中能量输运的大涡模拟

Hao Guo, P. Jiang, Yinhai Zhu
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引用次数: 0

摘要

采用大涡模拟方法研究了圆形层流射流在全湍流高马赫数横流中的热能输运和混合过程。本文系统地分析了高可压缩流体的能量方程,定量地比较了方程中各项的贡献。湍流焓输运与平均运动相关的平流项在同一个数量级,因此在考虑气膜冷却的对流换热问题时不可忽略,这与横流中不可压缩射流的研究结论不同。详细解释了反梯度焓输运引起的RANS湍流建模不准确的原因,并提出了一种更合理的三维分析方法,用于深入机理分析和湍流模型改进。数值结果还表明,在射流和横流相互作用和混合强烈的近场区域,平均运动对热能输运总动能耗散的贡献占主导地位,而在其他大部分区域,湍流动能耗散占主导地位。并对流场中耗散和换热引起的不可逆熵增进行了比较。结果表明,在处理高压涡轮中常见的大温差气膜冷却时,后者引起的熵产是不可忽视的。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
Large Eddy Simulation of Energy Transport in Highly Compressible Transverse Jets
Large eddy simulation is performed to study the thermal energy transport and mixing process of a round laminar jet in a fully-turbulent high-Mach-number crossflow. In this study, the energy equation of highly compressible fluid is systematically analyzed and the contributions of each term in the equation are compared quantitatively. Turbulent enthalpy transport is found to be in the same order of magnitude as the advection term associated with mean motion and thus is not negligible when considering the convective heat transfer problem of film cooling, which differs from the conclusion drawn from the incompressible-jets-in-crossflow studies. The inaccuracy of RANS turbulent modeling caused by counter-gradient transport of enthalpy is explained in detail and a more reasonable three-dimensional analysis method is proposed for in-depth mechanism analysis and turbulent model improvement. The numerical results also show that the contribution of mean motion to the overall kinetic energy dissipation in thermal energy transport is dominant in the near-field region where jets and crossflow interact and mix intensively while the turbulent kinetic energy dissipation term predominates in most other regions. Moreover, the irreversible increase in entropy caused by dissipation and heat transfer in the flow field is compared. The results show that the entropy production due to the latter one cannot be ignored when dealing with large temperature difference film cooling which is common in high-pressure turbines.
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